Hydraulics Flashcards

1
Q

How many hydraulic systems are on the airplane?

A

3 Independent systems: HYD 1, HYD 2, and HYD 3

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2
Q

What systems use hydraulic power?

A

Flight controls, Spoilers, Landing gear, Nose wheel steering, Wheel brakes, Thrust reversers

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3
Q

Can hydraulic fluid be transferred between each system?

A

No

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4
Q

How many hydraulic pumps are on the airplane?

A

7 total: 2 EDPs (Engine Driven Pumps), 4 ACMPs (AC Motor Pumps), 1 PTU

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5
Q

What are the basic components of the hydraulic systems?

A

Reservoir, Pumps, Accumulator

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6
Q

What is the purpose of the accumulator?

A

Helps to maintain constant pressure by covering transient demands and helps to avoid pump cavitation

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7
Q

When will ACMP 1 or 2 automatically activate?

A

Ground: Flaps > 0, and TL set to TOGA, OR Grounds > 50 kts (Remains on for 60 seconds after TL at TOGA);

Flight: Engine failure or EDP failure, OR Flaps > 0 (Remains on for 60 seconds after landing)

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8
Q

What are some important items controlled by HYD 2 system?

A

Landing gear, Nose wheel steering, Inboard brakes

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9
Q

What is the PTU?

A

Power Transfer Unit: Mechanical pump that uses HYD 1 power to provide HYD 2 pressure

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10
Q

What is the primary purpose of the PTU?

A

To allow landing gear retraction and extension in the event of an engine 2 or EDP 2 failure

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11
Q

When will the PTU automatically activate?

A

During takeoff and landing with flaps > 0, if Engine 2 fails, or EDP 2 fails.

(Must have above 12% quantity in #2 Hydraulic Reservoir and Airplane is Airborne. Engine #1 EDP must be operational.)

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12
Q

How is single engine taxi possible if nose wheel steering is on HYD 2?

A

Releasing the parking brake activates ACMP 2

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13
Q

What is the primary purpose of HYD 3 system?

A

Back-up for the Flight controls

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14
Q

Why does HYD ACMP 3A pump switch have an ON position and HYD ACMP 3B have an AUTO position?

A

HYD ACMP 3A pump is primary and has no automation; HYD ACMP 3B pump is a back-up and automatically activates if ACMP 3A fails with normal AC power

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15
Q

What, if any, HYD ACMP will function if the RAT is the only power source?

A

HYD ACMP 3A only with no backup

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16
Q

In an electrical emergency what provides hydraulic pressure to flight controls until the RAT comes online?

A

HYD 3 accumulator (After 8 seconds the RAT will power ACMP 3A)

17
Q

In an electrical emergency can HYD 3 system power requirements overload the RAT?

A

No. A flow limiter valve and a pump unloader valve are used to reduce flow and limits pump electrical power draw to prevent a RAT stall